FR3016605B1 - PART OF A FUSELAGE OF AN AIRCRAFT COMPRISING A VENTRAL BEAM AND A REAR LOWER HULL - Google Patents
PART OF A FUSELAGE OF AN AIRCRAFT COMPRISING A VENTRAL BEAM AND A REAR LOWER HULL Download PDFInfo
- Publication number
- FR3016605B1 FR3016605B1 FR1450507A FR1450507A FR3016605B1 FR 3016605 B1 FR3016605 B1 FR 3016605B1 FR 1450507 A FR1450507 A FR 1450507A FR 1450507 A FR1450507 A FR 1450507A FR 3016605 B1 FR3016605 B1 FR 3016605B1
- Authority
- FR
- France
- Prior art keywords
- fuselage
- aircraft
- rear lower
- lower hull
- ventral beam
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
- B64C1/061—Frames
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
- B64C1/12—Construction or attachment of skin panels
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
- B64C1/065—Spars
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C2001/0054—Fuselage structures substantially made from particular materials
- B64C2001/0072—Fuselage structures substantially made from particular materials from composite materials
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/40—Weight reduction
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1450507A FR3016605B1 (en) | 2014-01-22 | 2014-01-22 | PART OF A FUSELAGE OF AN AIRCRAFT COMPRISING A VENTRAL BEAM AND A REAR LOWER HULL |
US14/601,936 US9688377B2 (en) | 2014-01-22 | 2015-01-21 | Part of a fuselage of an aircraft and aircraft comprising a keel beam and an aft lower shell |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1450507A FR3016605B1 (en) | 2014-01-22 | 2014-01-22 | PART OF A FUSELAGE OF AN AIRCRAFT COMPRISING A VENTRAL BEAM AND A REAR LOWER HULL |
FR1450507 | 2014-01-22 |
Publications (2)
Publication Number | Publication Date |
---|---|
FR3016605A1 FR3016605A1 (en) | 2015-07-24 |
FR3016605B1 true FR3016605B1 (en) | 2018-01-26 |
Family
ID=50549102
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1450507A Active FR3016605B1 (en) | 2014-01-22 | 2014-01-22 | PART OF A FUSELAGE OF AN AIRCRAFT COMPRISING A VENTRAL BEAM AND A REAR LOWER HULL |
Country Status (2)
Country | Link |
---|---|
US (1) | US9688377B2 (en) |
FR (1) | FR3016605B1 (en) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US9505354B2 (en) * | 2013-09-16 | 2016-11-29 | The Boeing Company | Carbon fiber reinforced polymer cargo beam with integrated cargo stanchions and c-splices |
Family Cites Families (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5324563A (en) * | 1990-08-08 | 1994-06-28 | Bell Helicopter Textron Inc. | Unidirectional carbon fiber reinforced pultruded composite material having improved compressive strength |
US5619903A (en) * | 1994-11-30 | 1997-04-15 | Bell Helicopter Textron Inc. | Braided preform for composite bodies |
US8333858B2 (en) * | 2006-02-02 | 2012-12-18 | The Boeing Company | Method for fabricating curved thermoplastic composite parts |
FR2901240B1 (en) * | 2006-05-17 | 2009-01-09 | Airbus France Sas | COMPOSITE INTERNAL BEAM FOR STRENGTHENING THE STRUCTURE OF AN AIRCRAFT |
US9180960B2 (en) * | 2011-06-10 | 2015-11-10 | The Boeing Company | Boron fiber reinforced structural components |
US9090043B2 (en) * | 2011-08-03 | 2015-07-28 | The Boeing Company | Molybdenum composite hybrid laminates and methods |
US8703269B2 (en) * | 2012-02-14 | 2014-04-22 | Gulfstream Aerospace Corporation | Reinforced composite structures for aircrafts and methods for making the same |
US10099765B2 (en) * | 2012-08-08 | 2018-10-16 | The Boeing Company | Monolithic composite structures for vehicles |
US9399507B2 (en) * | 2014-01-22 | 2016-07-26 | The Boeing Company | Joints between a composite skin and a load-bearing component and methods of forming same |
-
2014
- 2014-01-22 FR FR1450507A patent/FR3016605B1/en active Active
-
2015
- 2015-01-21 US US14/601,936 patent/US9688377B2/en active Active
Also Published As
Publication number | Publication date |
---|---|
FR3016605A1 (en) | 2015-07-24 |
US20150225062A1 (en) | 2015-08-13 |
US9688377B2 (en) | 2017-06-27 |
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